FIELD: transport.
SUBSTANCE: invention relates to space engineering and may be used in deploying solar batteries of spacecrafts. Device for separation and opening of aircraft solar battery flaps (DSOSBF) includes frame, two packs of flaps, hold-down locks with hooks, rockers, spring-loaded tie rod with yokes interacting with upper flaps, spring-loaded rods with through holes for pin with butt ends interacting with profiled grooves, retaining rings with retainers.
EFFECT: higher reliability, decreased dimensions of DSOSBF.
8 dwg
Title | Year | Author | Number |
---|---|---|---|
UNIT OFFICES AND OPENING THE VALVES OF SOLAR BATTERIES OF SPACECRAFT | 2010 |
|
RU2441817C1 |
LOCKING DEVICE FOR TEMPERATURE ISOLATION | 2020 |
|
RU2753015C1 |
SOLAR CELL PANEL FOR SPACECRAFT | 2010 |
|
RU2460676C2 |
SPACECRAFT SOLAR BATTERY | 2001 |
|
RU2221731C2 |
SPACECRAFT SOLAR PANEL | 2015 |
|
RU2619158C2 |
CARRIER ROCKET DETACHABLE NOSE CONE | 2010 |
|
RU2428359C1 |
SOLAR BATTERY OPENING TEST BENCH | 2010 |
|
RU2468969C2 |
SPACECRAFT SOLAR BATTERY | 2002 |
|
RU2214949C1 |
SPACECRAFT SOLAR BATTERY | 1998 |
|
RU2167793C2 |
SELF-OPENING SOLAR BATTERY PANEL OF SPACE VEHICLE | 0 |
|
SU1763293A1 |
Authors
Dates
2015-06-27—Published
2013-09-16—Filed